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Wind tunnel interference on unsteady two-dimensional aerofoil motions in low speed flows

Published online by Cambridge University Press:  04 July 2016

C. W. Cheung
Affiliation:
Department of Aeronautical Engineering, Queen Mary College
G. J. Hancock
Affiliation:
Department of Aeronautical Engineering, Queen Mary College

Summary

The aerodynamic characteristics of two-dimensional transient aerofoil motions in low-speed flows in a wind tunnel with either closed wall or open (jet) walls, including the effect of a downstream closed wall diffuser, have been investigated. The mathematical formulation for the aerofoil and its unsteady wake is based on linear theory and is solved by a piecewise linear vorticity method; the wall boundaries are represented by distributions of sources. Numerical calculations have been made for various values of tunnel height to chord ratio.

Interference effects on the rate of build up of lift to a steady state following a step change in incidence can be large, especially for open jet tunnels.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1988 

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References

1. Garner, H. C. Subsonic wind tunnel wall corrections. AGAR-Dograph 109, 1966.Google Scholar
2. Sasaki, T. On the effect of wall on a wind tunnel upon the lift coefficient of a model. Aero Res Inst (Tokyo) Report 46, 1928.Google Scholar
3. Tomotika, S. The lift of a flat plate placed in a stream between two parallel walls and some allied problems. Aero Res Inst (Toyko) Report 101, 1934.Google Scholar
4. Katzoff, S. Linear theory of boundary effects in open wind tunnels with finite jet lengths. NACA Report 976, 1950.Google Scholar